您当前的位置:
首页 >
文章列表页 >
A new method to control fuel flow of aircraft engine's starting process based on PSO Algorithm
更新时间:2026-07-07
    • A new method to control fuel flow of aircraft engine's starting process based on PSO Algorithm

    • Vol. 22, Issue 6, (2007)
    • Published:2007

    移动端阅览

  • ZHANG Dong-fang, LI Ying-hong, CHEN Dong-lin. A new method to control fuel flow of aircraft engine's starting process based on PSO Algorithm[J]. 2007, 22(6). DOI:

  •  
  •  
icon
试读结束,您可以激活您的VIP账号继续阅读。
去激活 >
icon
试读结束,您可以通过登录账户,到个人中心,购买VIP会员阅读全文。
已是VIP会员?
去登录 >

0

Views

487

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

Experimental study of flow characteristics of inlet /internal flowpath for a hypersonic flight vehicle
Critical starting characteristics of hypersonic inlets
A prediction model of film-cooling adiabatic effectiveness based on cohence non-isothermal jet theory
Design and numerical simulation of a transonic swept fan
Effect of inclined angle on discharge coefficient of the discrete holes in curved wall

Related Author

WANG Cheng-peng
ZHANG Hong-ying
SUN Shu
WANG Jiang-feng
CHENG Ke-ming
ZHANG Chi
LIN Yu-zhen
XU Quan-hong

Related Institution

College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics
National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
The key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Ministry of Education, Northwestern Polytechnical University
China Aerospace Science and Technology Corporation
National Key Laboratory on Aero-Engins, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
0